Add axial points to a design to estimate the square terms for factors. You can add axial points to 2-level factorial designs and Plackett-Burman designs, if those designs have only continuous factors. This modification changes the design from a factorial design to a central composite response surface design. For more information, go to What are response surface designs, central composite designs, and Box-Behnken designs?.
Alpha (α) is the distance, in coded units, of each axial point (also called star point) from the center in a central composite design. Alpha, along with the number of center points, determines whether a design can be orthogonally blocked and is rotatable. For more information, go to What is alpha (α) in a central composite design?. Choose one of the following to specify the value of alpha:
For example, an engineer plans a sequential experiment and begins with a 2-level factorial design. The analysis of that design suggests that the relationship between the factors and the response variable has curvature. The engineer then uses Modify Design to add axial points to the design to add runs to model the curvature.
C1 | C2 | C3 | C4 | C5 | C6 | C7 | C8 |
---|---|---|---|---|---|---|---|
StdOrder | RunOrder | CenterPt | Blocks | Pressure | Injection | Cooling | Strength |
4 | 1 | 1 | 1 | 150.000 | 100.000 | 50.0000 | 22.7001 |
1 | 2 | 1 | 1 | 75.000 | 85.000 | 50.0000 | 5.7349 |
2 | 3 | 1 | 1 | 150.000 | 85.000 | 25.0000 | 22.7105 |
6 | 4 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 12.8237 |
7 | 5 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 18.8239 |
3 | 6 | 1 | 1 | 75.000 | 100.000 | 25.0000 | 5.7751 |
5 | 7 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 12.8233 |
C1 | C2 | C3 | C4 | C5 | C6 | C7 | C8 |
---|---|---|---|---|---|---|---|
StdOrder | RunOrder | CenterPt | Blocks | Pressure | Injection | Cooling | Strength |
4 | 1 | 1 | 1 | 150.000 | 100.000 | 50.0000 | 22.7001 |
1 | 2 | 1 | 1 | 75.000 | 85.000 | 50.0000 | 5.7349 |
2 | 3 | 1 | 1 | 150.000 | 85.000 | 25.0000 | 22.7105 |
6 | 4 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 12.8237 |
7 | 5 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 18.8239 |
3 | 6 | 1 | 1 | 75.000 | 100.000 | 25.0000 | 5.7751 |
5 | 7 | 0 | 1 | 112.500 | 92.500 | 37.5000 | 12.8233 |
8 | 8 | −1 | 2 | 59.467 | 92.500 | 37.5000 | |
9 | 9 | −1 | 2 | 165.533 | 92.500 | 37.5000 | |
10 | 10 | −1 | 2 | 112.500 | 81.893 | 37.5000 | |
11 | 11 | −1 | 2 | 112.500 | 103.107 | 37.5000 | |
12 | 12 | −1 | 2 | 112.500 | 92.500 | 19.8223 | |
13 | 13 | −1 | 2 | 112.500 | 92.500 | 55.1777 |